[go: up one dir, main page]

US4236573A - High-temperature gas exit from a pre-stressed pressure container - Google Patents

High-temperature gas exit from a pre-stressed pressure container Download PDF

Info

Publication number
US4236573A
US4236573A US05/960,833 US96083378A US4236573A US 4236573 A US4236573 A US 4236573A US 96083378 A US96083378 A US 96083378A US 4236573 A US4236573 A US 4236573A
Authority
US
United States
Prior art keywords
cooling
temperature gas
gas exit
casing
wall
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/960,833
Inventor
Rolf Dorling
Hans Hemshemeier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Zosen Inova Steinmueller GmbH
Original Assignee
L&C Steinmueller GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by L&C Steinmueller GmbH filed Critical L&C Steinmueller GmbH
Application granted granted Critical
Publication of US4236573A publication Critical patent/US4236573A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C11/00Shielding structurally associated with the reactor
    • G21C11/08Thermal shields; Thermal linings, i.e. for dissipating heat from gamma radiation which would otherwise heat an outer biological shield ; Thermal insulation
    • G21C11/088Thermal shields; Thermal linings, i.e. for dissipating heat from gamma radiation which would otherwise heat an outer biological shield ; Thermal insulation consisting of a stagnant or a circulating fluid
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C13/00Pressure vessels; Containment vessels; Containment in general
    • G21C13/02Details
    • G21C13/032Joints between tubes and vessel walls, e.g. taking into account thermal stresses
    • G21C13/036Joints between tubes and vessel walls, e.g. taking into account thermal stresses the tube passing through the vessel wall, i.e. continuing on both sides of the wall
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors

Definitions

  • the present invention relates to a high-temperature gas exit in the shape of pipe bundles from a pre-stressed pressure container designed as cast or concrete structure which is provided with a cooling system located on the inner side of the perpretration and comprises a sealing skin with cooling pipes arranged on the outside thereof and with a thermal insulation layer arranged on the inner side thereof.
  • FIG. 1 diagrammatically illustrates a high temperature gas exit according to the invention in the form of a pipe bundle or pipe assembly with a concrete mantle.
  • FIG. 2 represents a horizontal section taken along the line II--II of FIG. 1 but on a larger scale than that of FIG. 1.
  • the high temperature gas exit according to the present invention is characterized primarily in that between a first cooling system and the pipe bundle or pipe assembly there is provided a second cooling system comprising a hollow double skin with cooling passages, the first cooling system and the second cooling system being independent of each other.
  • the high-temperature gas exit comprises a pipe bundle or pipe assembly 1.
  • the thermal screening toward the outside is effected by a first cooling system which comprises a sealing skin or sealing casing 2 with cooling pipes 3 located on the outside of the sealing skin, and an insulating layer 4 on the inside of said sealing skin 2.
  • the sealing skin or sealing casing 2 surrounds the pipe bundle or pipe assembly 1 and is in sealing engagement with the surface of the opening through which the pipe bundle passes.
  • the sealing casing 2 has a portion 2a which extends past the wall.
  • the cooling pipes 3 are also positioned around the portion 2a which extends past the wall.
  • This first cooling system is according to the invention supplemented by a second cooling system which comprises a hollow double skin or jacket 5 with cooling passages 6 which double skin 5 surrounds the pipe bundle 1 in close proximity thereto. There is a space between the hollow double skin 5 or jacket and the insulating layer 4.
  • the cylindrical surface x which defines the opening y through the wall z is shielded from the heat eminating from pipe bundle 1.
  • cooling medium inlet conduits 7 and two cooling medium outlet conduits 8 are provided at least two cooling medium inlet conduits 7 and two cooling medium outlet conduits 8.
  • these cooling medium inlet and outlet conduits 7 and 8 are coupled to an additional high-temperature gas exit with a corresponding cooling system as mentioned above, corresponding to the first and second cooling systems and coupled to the at least two inlet and outlet conduits 7, 8.
  • the cooling medium inlet and outlet conduits 7, 8 comprise double walled pipes so that in the interior there flows the high-temperature gas and in the outer high-temperature passage there flows the cooling medium.
  • the high-temperature gas exit according to the invention assures the required safety screen relative to the atmosphere.
  • the high-temperature gas exit in the form of a pipe assembly is in conformity with the heat flow relative to its mantle of concrete or cast material screened in such a way that harmful heat overloads will no longer occur. This has a favorable effect upon the supporting capability of the concrete mantle as well as upon the frictional stresses exerted upon the sealing skin.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Biomedical Technology (AREA)
  • General Health & Medical Sciences (AREA)
  • Molecular Biology (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
  • Building Environments (AREA)

Abstract

A high-temperature gas exit in the form of a pipe bundle from a pre-stressed cast or concrete pressure container with a first cooling system comprising a sealing skin having cooling pipes arranged on the outside thereof and with a thermal insulation layer arranged on the inner side of the sealing skin. Between the first cooling system and the pipe bundle there is provided a second cooling system comprising a hollow double skin with cooling passages, the first cooling system and the second cooling system being independent of each other.

Description

The present invention relates to a high-temperature gas exit in the shape of pipe bundles from a pre-stressed pressure container designed as cast or concrete structure which is provided with a cooling system located on the inner side of the perpretration and comprises a sealing skin with cooling pipes arranged on the outside thereof and with a thermal insulation layer arranged on the inner side thereof.
With gas exits or gas discharges of the above mentioned type, there exists now as before the problem of an insufficient heat accumulation in the direction toward the concrete or cast mantle. This causes intolerable temperature loads, especially in the concrete mantle.
It is, therefore, an object of the present invention with high-temperature gas exits, so to design the there existing cooling system that during operation, the temperature load of the concrete or cast mantle of the exit or outlet be kept in permissible limits.
These and other objects and advantages of the invention will appear more clearly from the following specification in connection with the accompanying drawings, in which:
FIG. 1 diagrammatically illustrates a high temperature gas exit according to the invention in the form of a pipe bundle or pipe assembly with a concrete mantle.
FIG. 2 represents a horizontal section taken along the line II--II of FIG. 1 but on a larger scale than that of FIG. 1.
The high temperature gas exit according to the present invention is characterized primarily in that between a first cooling system and the pipe bundle or pipe assembly there is provided a second cooling system comprising a hollow double skin with cooling passages, the first cooling system and the second cooling system being independent of each other.
Referring now to the drawings in detail, the high-temperature gas exit comprises a pipe bundle or pipe assembly 1. The thermal screening toward the outside is effected by a first cooling system which comprises a sealing skin or sealing casing 2 with cooling pipes 3 located on the outside of the sealing skin, and an insulating layer 4 on the inside of said sealing skin 2. As is seen in FIG. 1, the sealing skin or sealing casing 2 surrounds the pipe bundle or pipe assembly 1 and is in sealing engagement with the surface of the opening through which the pipe bundle passes. Moreover, the sealing casing 2 has a portion 2a which extends past the wall. The cooling pipes 3 are also positioned around the portion 2a which extends past the wall. This first cooling system is according to the invention supplemented by a second cooling system which comprises a hollow double skin or jacket 5 with cooling passages 6 which double skin 5 surrounds the pipe bundle 1 in close proximity thereto. There is a space between the hollow double skin 5 or jacket and the insulating layer 4. By the aforedescribed structure, the cylindrical surface x which defines the opening y through the wall z is shielded from the heat eminating from pipe bundle 1.
There are provided at least two cooling medium inlet conduits 7 and two cooling medium outlet conduits 8. In the specific embodiment shown in the drawings, these cooling medium inlet and outlet conduits 7 and 8 are coupled to an additional high-temperature gas exit with a corresponding cooling system as mentioned above, corresponding to the first and second cooling systems and coupled to the at least two inlet and outlet conduits 7, 8. The cooling medium inlet and outlet conduits 7, 8 comprise double walled pipes so that in the interior there flows the high-temperature gas and in the outer high-temperature passage there flows the cooling medium.
As will be evident from the above, the high-temperature gas exit according to the invention assures the required safety screen relative to the atmosphere.
More specifically, the high-temperature gas exit in the form of a pipe assembly is in conformity with the heat flow relative to its mantle of concrete or cast material screened in such a way that harmful heat overloads will no longer occur. This has a favorable effect upon the supporting capability of the concrete mantle as well as upon the frictional stresses exerted upon the sealing skin.
It is, of course, to be understood that the present invention is, by no means, limited to the specific showing in the drawings, but also comprises any modifications within the scope of the appended claims.

Claims (2)

What we claim is:
1. A high temperature gas exit conduit in the form of a pipe bundle means in combination with and extending through an opening in a wall of a pre-stressed, concrete pressure container, the combination comprising:
a surface defined by the opening, said surface extending through the thickness of the wall;
a casing surrounding the bundle and in sealing engagement with the entire surface of the opening, said casing having a portion extending past the wall;
cooling pipe means disposed both between the surface of the opening and the casing on that portion of the casing extending past the wall;
a layer of thermal insulation lining the entire inner surface of the casing and surrounding the pipe bundle, and
additional cooling means, independent of said cooling pipe means, and surrounding and in close proximity to the pipe bundle means, said additional cooling means being in spaced relation to the layer of thermal insulation.
2. A high-temperature gas exit according to claim 1, which includes in combination: at least two inlet conduits and two outlet conduits for a cooling medium, said inlet and outlet conduits comprising double walled pipes, and an additional high-temperature gas exit comprising a cooling arrangement corresponding to said first and second cooling systems and coupled to said at least two inlet and outlet conduits.
US05/960,833 1977-11-15 1978-11-15 High-temperature gas exit from a pre-stressed pressure container Expired - Lifetime US4236573A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2750968 1977-11-15
DE2750968A DE2750968C2 (en) 1977-11-15 1977-11-15 High-temperature gas outlet in the form of a tube bundle from a pre-stressed pressure vessel in GuB or concrete construction

Publications (1)

Publication Number Publication Date
US4236573A true US4236573A (en) 1980-12-02

Family

ID=6023763

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/960,833 Expired - Lifetime US4236573A (en) 1977-11-15 1978-11-15 High-temperature gas exit from a pre-stressed pressure container

Country Status (4)

Country Link
US (1) US4236573A (en)
CH (1) CH637196A5 (en)
DE (1) DE2750968C2 (en)
FR (1) FR2408804A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4587082A (en) * 1980-08-08 1986-05-06 Hochtemperatur-Reaktorbau Gmbh Passage through the wall of a reinforced concrete pressure vessel
US4976913A (en) * 1989-04-24 1990-12-11 Schoessow Glen J Nuclear energy system using pelletized fuel in a boiling liquid reactor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3126422C2 (en) * 1981-07-04 1985-06-13 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8500 Nürnberg Device to compensate for different thermal expansion and to seal multi-way tubular heat exchangers

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB619158A (en) * 1945-12-18 1949-03-04 Sulzer Ag Improvements relating to gas heaters
US3000364A (en) * 1957-01-30 1961-09-19 Babcock & Wilcox Co Reactor with superheater coil encircling heat carrier lift pipe
US3059908A (en) * 1959-09-29 1962-10-23 Iii Thomas H Fox Heat exchanger
US3301320A (en) * 1964-08-07 1967-01-31 Pyrochem Corp Apparatus for containing hot metalattacking gases such as hydrogen and hydrogen sulphide under pressure whereby chemical and thermal stresses are separated from hoop stress
US3357890A (en) * 1966-11-21 1967-12-12 Ronald W Friis Pressure vessel thermal insulation
US3443631A (en) * 1963-09-19 1969-05-13 Beteiligungs & Patentverw Gmbh High-pressure container
US3497421A (en) * 1968-01-15 1970-02-24 Commissariat Energie Atomique Shielded enclosure providing resistance to high temperatures and pressures
US3834452A (en) * 1971-04-21 1974-09-10 Commissariat En Atomique And E Removable head pressure vessel, especially for boiling-water reactors
DE2753796A1 (en) * 1976-12-16 1978-06-29 Westinghouse Electric Corp HEAT EXCHANGERS, IN PARTICULAR FOR NUCLEAR REACTOR SYSTEMS, WITH AN AUXILIARY COOLING DEVICE

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1041042A (en) * 1961-11-08 1966-09-01 Babcock & Wilcox Ltd Improvements in concrete walls
FR2041724A1 (en) * 1969-05-13 1971-02-05 Ind Atomique S O C I A Soc Pou Gas circuit for gas cooled nuclear reactor
CH576097A5 (en) * 1974-12-18 1976-05-31 Sulzer Ag

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB619158A (en) * 1945-12-18 1949-03-04 Sulzer Ag Improvements relating to gas heaters
US3000364A (en) * 1957-01-30 1961-09-19 Babcock & Wilcox Co Reactor with superheater coil encircling heat carrier lift pipe
US3059908A (en) * 1959-09-29 1962-10-23 Iii Thomas H Fox Heat exchanger
US3443631A (en) * 1963-09-19 1969-05-13 Beteiligungs & Patentverw Gmbh High-pressure container
US3301320A (en) * 1964-08-07 1967-01-31 Pyrochem Corp Apparatus for containing hot metalattacking gases such as hydrogen and hydrogen sulphide under pressure whereby chemical and thermal stresses are separated from hoop stress
US3357890A (en) * 1966-11-21 1967-12-12 Ronald W Friis Pressure vessel thermal insulation
US3497421A (en) * 1968-01-15 1970-02-24 Commissariat Energie Atomique Shielded enclosure providing resistance to high temperatures and pressures
US3834452A (en) * 1971-04-21 1974-09-10 Commissariat En Atomique And E Removable head pressure vessel, especially for boiling-water reactors
DE2753796A1 (en) * 1976-12-16 1978-06-29 Westinghouse Electric Corp HEAT EXCHANGERS, IN PARTICULAR FOR NUCLEAR REACTOR SYSTEMS, WITH AN AUXILIARY COOLING DEVICE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4587082A (en) * 1980-08-08 1986-05-06 Hochtemperatur-Reaktorbau Gmbh Passage through the wall of a reinforced concrete pressure vessel
US4976913A (en) * 1989-04-24 1990-12-11 Schoessow Glen J Nuclear energy system using pelletized fuel in a boiling liquid reactor

Also Published As

Publication number Publication date
DE2750968C2 (en) 1979-03-29
CH637196A5 (en) 1983-07-15
FR2408804A1 (en) 1979-06-08
FR2408804B1 (en) 1983-07-29
DE2750968B1 (en) 1978-08-03

Similar Documents

Publication Publication Date Title
US3863445A (en) Heat shields for exhaust system
CN102015971A (en) Burner holding device comprising a cooling system for a burner arrangement in an entrained bed gasifier
US4259993A (en) Ceramic-insulated pipe for the transport of hot fluids
US4252212A (en) Muffler for combustion engines
US3159238A (en) Diffuser screen with heat-insulating rungs for exhaust noise suppressor for reactionengines
US4483140A (en) Exhaust gas conduit system for multi-cylinder reciprocating piston internal combustion engines
US3705734A (en) Arrangement for compensating for changes in the length of pipes and the like
US4033381A (en) Hot air duct
US5012860A (en) Actively cooled heat protective shield
US4236573A (en) High-temperature gas exit from a pre-stressed pressure container
CA1175231A (en) Connection joint of a reaction vessel in a gasification plant
US3952777A (en) Hollow body for heated gases
US4582094A (en) Insulation for hot gas piping
JPS5921000B2 (en) nuclear reactor equipment
US2866617A (en) Shielded gas turbine
US3963223A (en) Metallurgical vessel, in particular a converter
CA1087838A (en) Rotary kiln
US4369163A (en) Thermal shielding for bottoms and covers of reaction vessels
US4268017A (en) Reactor with extractable feed nozzle
JPS5844717B2 (en) Reactor for gas production by partial oxidation
CS209534B2 (en) Elbow for exhausting the gas waste products
US3314668A (en) Blast furnace stack with cooling staves
US4296776A (en) Gate valve for use in large size conduits
GB2048445A (en) A water cooled cover for an industrial furnace
US4118276A (en) Conduit system for gases of high temperature and high pressure